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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 14 15 16 17 18 Next > Last >>
EPPLER 361 12.09 1.695 27.98 1.116 0.0157
EPPLER 374 10.91 2.315 38.94 1.126 0.0066
EPPLER 378 4.08 8.109 35.92 1.686 0.0014
EPPLER 387 9.07 3.797 40.08 1.199 0.0064
EPPLER 397 13.5 5.331 52.1 1.47 0.0017
Coordinates
XUpper YUpper XLower YLower
0 -0.06 0 0.09
0.04 0.33 0.02 -0.2
0.11 0.6 0.03 -0.27
0.61 1.5 0.05 -0.34
1.53 2.43 0.08 -0.4
2.86 3.33 0.12 -0.45
4.61 4.17 0.16 -0.51
6.79 4.92 0.21 -0.57
9.42 5.57 0.34 -0.68
12.46 6.15 0.49 -0.79
15.88 6.64 0.76 -0.96
19.64 7.05 1.58 -1.34
23.69 7.37 3.22 -1.86
27.98 7.58 5.37 -2.33
32.47 7.66 8.03 -2.77
37.12 7.61 11.14 -3.16
41.89 7.39 14.68 -3.51
46.78 7.01 18.6 -3.81
51.76 6.49 22.85 -4.07
56.81 5.87 27.39 -4.27
61.86 5.19 32.17 -4.41
66.85 4.49 37.12 -4.49
71.73 3.78 42.2 -4.51
76.42 3.1 47.34 -4.47
80.85 2.47 52.5 -4.35
84.96 1.9 57.61 -4.15
88.68 1.41 62.65 -3.87
91.95 0.99 67.56 -3.51
92.01 0.9882 72.32 -3.09
94.7 0.65 76.87 -2.62
96.92 0.36 81.17 -2.15
98.58 0.14 85.17 -1.68
99.63 0.02 88.8 -1.26
100 0 92.01 -0.89
X Y
1 0
0.9963 0.0002
0.9858 0.0014
0.9692 0.0036
0.947 0.0065
0.9201 0.009882
0.9195 0.0099
0.8868 0.0141
0.8496 0.019
0.8085 0.0247
0.7642 0.031
0.7173 0.0378
0.6685 0.0449
0.6186 0.0519
0.5681 0.0587
0.5176 0.0649
0.4678 0.0701
0.4189 0.0739
0.3712 0.0761
0.3247 0.0766
0.2798 0.0758
0.2369 0.0737
0.1964 0.0705
0.1588 0.0664
0.1246 0.0615
0.0942 0.0557
0.0679 0.0492
0.0461 0.0417
0.0286 0.0333
0.0153 0.0243
0.0061 0.015
0.0011 0.006
0.0004 0.0033
0 -0.0006
0 0.0009
0.0002 -0.002
0.0003 -0.0027
0.0005 -0.0034
0.0008 -0.004
0.0012 -0.0045
0.0016 -0.0051
0.0021 -0.0057
0.0034 -0.0068
0.0049 -0.0079
0.0076 -0.0096
0.0158 -0.0134
0.0322 -0.0186
0.0537 -0.0233
0.0803 -0.0277
0.1114 -0.0316
0.1468 -0.0351
0.186 -0.0381
0.2285 -0.0407
0.2739 -0.0427
0.3217 -0.0441
0.3712 -0.0449
0.422 -0.0451
0.4734 -0.0447
0.525 -0.0435
0.5761 -0.0415
0.6265 -0.0387
0.6756 -0.0351
0.7232 -0.0309
0.7687 -0.0262
0.8117 -0.0215
0.8517 -0.0168
0.888 -0.0126
0.9201 -0.0089
X Y
100 0
99.63 0.02
98.58 0.14
96.92 0.36
94.7 0.65
92.01 0.9882
91.95 0.99
88.68 1.41
84.96 1.9
80.85 2.47
76.42 3.1
71.73 3.78
66.85 4.49
61.86 5.19
56.81 5.87
51.76 6.49
46.78 7.01
41.89 7.39
37.12 7.61
32.47 7.66
27.98 7.58
23.69 7.37
19.64 7.05
15.88 6.64
12.46 6.15
9.42 5.57
6.79 4.92
4.61 4.17
2.86 3.33
1.53 2.43
0.61 1.5
0.11 0.6
0.04 0.33
0 -0.06
0 0.09
0.02 -0.2
0.03 -0.27
0.05 -0.34
0.08 -0.4
0.12 -0.45
0.16 -0.51
0.21 -0.57
0.34 -0.68
0.49 -0.79
0.76 -0.96
1.58 -1.34
3.22 -1.86
5.37 -2.33
8.03 -2.77
11.14 -3.16
14.68 -3.51
18.6 -3.81
22.85 -4.07
27.39 -4.27
32.17 -4.41
37.12 -4.49
42.2 -4.51
47.34 -4.47
52.5 -4.35
57.61 -4.15
62.65 -3.87
67.56 -3.51
72.32 -3.09
76.87 -2.62
81.17 -2.15
85.17 -1.68
88.8 -1.26
92.01 -0.89
V 1.1